论文信息 - Design, development, and testing of a shrouded single-rotor micro air vehicle with antitorque vanes - 字舞流文

Design, development, and testing of a shrouded single-rotor micro air vehicle with antitorque vanes

Inderjit Chopra | Jayant Sirohi | Vikram Hrishikeshavan | Marat N. Tishchenko

[1] Mehdi Sabzehparvar. In-Flight Thrust Measurements of Propeller-Driven Airplanes , 2005 .

[2] Darryll J. Pines,et al. Small Rotor Design Optimization Using Blade Element Momentum Theory and Hover Tests , 2010 .

[3] Chopra,et al. Design and Testing of a Micro-Aerial Vehicle with a Single Rotor and Turning Vanes , 2005 .

[4] Inderjit Chopra,et al. Hover Tests of Micro Aerial Vehicle-Scale Shrouded Rotors, Part I: Performance Characteristics , 2009 .

[5] Rene´ Mouille. The “Fenestron,” Shrouded Tail Rotor of the SA. 341 Gazelle , 1970 .

[6] Benjamin Hein,et al. Hover Performance of a Micro Air Vehicle: Rotors at Low Reynolds Number , 2007 .

[7] J. Gordon Leishman,et al. Principles of Helicopter Aerodynamics , 2000 .

[8] Thomas J. Mueller,et al. Fixed and Flapping Wing Aerodynamics for Micro Air Vehicle Applications , 2001 .

[9] Vinod K. Lakshminarayan,et al. Computational investigation of micro-scale coaxial rotor aerodynamics in hover , 2010 .

[10] Dave Walsh,et al. The Sikorsky Cypher UAV: A Multi-Purpose Platform With Demonstrated Mission Flexibility , 1998 .

[11] A. H. Sacks,et al. Ducted Propellers—a Critical Review of the State of the Art , 1962 .

[12] Theodore R. Goodman. The Tip Correction for Wind-Tunnel Tests of Propellers , 1956 .